Twin Engine Turboprops
For several decades the Beech King Air family has reigned supreme in the twin turboprop segment, and for good reason. Operating economics are superb compared with a jet, as is the carrying capability of these models. While King Airs today don't sell nearly as well as they once did, a large pool of used airplanes and performance upgrades make them popular choices among pre-owned airplane buyers.
Piaggio Aero
Viking Air
Vulcanair
Beechcraft
King Air C90GTx
Base Price | $154,900 | Typically Equipped Price | $159,245 |
Engine | Lycoming O-235-K2C | Horsepower | 118 hp |
Propeller | Sensenich (2 blade) | Seats | 2 |
Length | 22 ft. 1 in. | Height | 7 ft. 8 in. |
Wingspan | 33 ft. 6 in. | Wing Area | 165 sq. ft. |
Wing Loading | 10.6 lb./sq. ft. | Power Loading | 14 lb./hp |
Max Takeoff Weight | 1,750 lb. | Empty Weight | 1,120 lb. |
Useful Load | 630 lb. | Fuel Capacity | 36 gal. |
Max Operating Altitude | 11,500 ft. | Max Rate of Climb | 704 fpm |
Max Cruise Speed | 104 kias | Normal Cruise Speed | 100 ktas |
Never Exceed Speed | 141 kias | Stall Speed, Flaps Up | 45 kcas |
Stall Speed, Landing Configuration | 43 kcas | Max Range | 595 nm |
Takeoff Roll | 650 ft. | Takeoff Distance Over 50 ft. | 1,050 ft. |
Landing Roll | 520 ft. | Landing Distance Over 50 ft. | 885 ft. |
Back to Top |
Beechcraft
King Air 250
Base Price | $6.39 million | Typically Equipped Price | N/A |
Engines | P&WC PT6A-52 | Horsepower Per Side | 850 shp |
Propellers | Hartzell (4 blade) | Seats | 10 |
Length | 43 ft. 10 in. | Height | 14 ft. 10 in. |
Wingspan | 57 ft. 11 in. | Wing Area | 310 sq. ft. |
Wing Loading | 40.3 lb./sq. ft. | Power Loading | 7.35 lb./shp |
Max Takeoff Weight | 12,500 lb. | Empty Weight | 8,830 lb. |
Useful Load | 3,760 lb. | Fuel Capacity | 544 gal./3,645 lb. |
Max Operating Altitude | 35,000 ft. | Max Rate of Climb | 2,450 fpm |
Single Engine Rate of Climb | 682 fpm | Max Cruise Speed | 310 ktas |
Normal Cruise Speed | 303 ktas | Stall Speed, Landing Configuration | 80 kcas |
Max Range | 1,720 nm | Takeoff Roll | 1,713 ft. |
Takeoff Distance Over 50 ft. | 2,111 ft. | Landing Roll | 1,750 ft. |
Landing Distance Over 50 ft. | 2,845 ft. | ||
Back to Top |
Beechcraft
King Air 350i
Base Price | $7.755 million | Typically Equipped Price | N/A |
Engines | P&WC PT6A-60A | Horsepower Per Side | 1,050 shp |
Propellers | Hartzell (4 blade) | Seats | 11 |
Length | 46 ft. 8 in. | Height | 14 ft. 4 in. |
Wingspan | 57 ft. 11. | Wing Area | 310 sq. ft. |
Wing Loading | 48.4 lb./sq. ft. | Power Loading | 7.14 lb./shp |
Max Takeoff Weight | 15,000 lb. | Empty Weight | 9,995 lb. |
Useful Load | 5,145 lb. | Fuel Capacity | 539 gal./3,611 lb. |
Max Operating Altitude | 35,000 ft. | Max Rate of Climb | 2,731 fpm |
Single Engine Rate of Climb | 552 fpm | Max Cruise Speed | 312 ktas |
Normal Cruise Speed | 308 ktas | Stall Speed, Landing Configuration | 82 kcas |
Max Range | 1,806 nm | Takeoff Roll | N/A |
Takeoff Distance Over 50 ft. | 3,300 ft. | Landing Roll | N/A |
Landing Distance Over 50 ft. | 2,692 ft. | ||
Back to Top |
Beechcraft
King Air 350ER
Base Price | $8.33 million | Typically Equipped Price | N/A |
Engines | P&WC PT6A-60A | Horsepower Per Side | 1,050 shp |
Propellers | Hartzell (4 blade) | Seats | 11 |
Length | 46 ft. 8 in. | Height | 14 ft. 4 in. |
Wingspan | 57 ft. 11. | Wing Area | 310 sq. ft. |
Wing Loading | 53.2 lb./sq. ft. | Power Loading | 7.86 lb./shp |
Max Takeoff Weight | 16,500 lb. | Empty Weight | 9,455 lb. |
Useful Load | 7,145 lb. | Fuel Capacity | 775 gal./5,192 lb. |
Max Operating Altitude | 35,000 ft. | Max Rate of Climb | 2,400 fpm |
Single Engine Rate of Climb | 337 fpm | Max Cruise Speed | 303 ktas |
Normal Cruise Speed | 198 ktas | Stall Speed, Landing Configuration | 82 kcas |
Max Range | 2,692 nm | Takeoff Roll | N/A |
Takeoff Distance Over 50 ft. | 4,057 ft. | Landing Roll | N/A |
Landing Distance Over 50 ft. | 2,728 ft. | ||
Back to Top |
Piaggio Aero
P180 Avanti Evo
Base Price | $7.695 million | Typically Equipped Price | N/A |
Engines | P&WC PT6A-66B | Horsepower Per Side | 850 shp |
Propellers | Hartzell (5 blade) | Seats | 10 |
Length | 47 ft. 3 in. | Height | 13 ft. 1 in. |
Wingspan | 47 ft. 1 in. | Wing Area | 172 sq. ft. |
Wing Loading | 70.3 lb./sq. ft. | Power Loading | 7.12 lb./shp |
Max Takeoff Weight | 12,100 lb. | Empty Weight | 7,850 lb. |
Useful Load | 4,100 lb. | Fuel Capacity | 400 gal./2,680 lb. |
Max Operating Altitude | 41,000 ft. | Max Rate of Climb | 2,600 fpm |
Single Engine Rate of Climb | 670 fpm | Max Cruise Speed | 402 ktas |
Normal Cruise Speed | 356 ktas | Stall Speed, Landing Configuration | 93 kcas |
Max Range | 1,470 nm | Takeoff Roll | 2,257 ft. |
Takeoff Distance Over 50 ft. | 3,262 ft. | Landing Roll | 2,300 ft. |
Landing Distance Over 50 ft. | 3,282 ft. | ||
Back to Top |
Viking Air
DHC-6-400 Twin Otter
Base Price | $6.5 million (est.) | Typically Equipped Price | $6.5 million (est.) |
Engines | P&WC PT6A-34 | Horsepower Per Side | 620 shp |
Propellers | Hartzell (3 blade) | Seats | 21 |
Length | 51 ft. 9 in. | Height | 19 ft. 6 in. |
Wingspan | 65 ft. | Wing Area | 420 sq. ft. |
Wing Loading | 29.8 lb./sq. ft. | Power Loading | 10.08 lb./shp |
Max Takeoff Weight | 12,500 lb. | Empty Weight | 5,851 lb. |
Useful Load | 4,425 lb. | Fuel Capacity | 378 gal./2,532 lb. |
Max Operating Altitude | 25,000 ft. | Max Rate of Climb | 1,500 fpm |
Single Engine Rate of Climb | 300 fpm | Max Cruise Speed | 182 ktas |
Normal Cruise Speed | 170 ktas | Stall Speed, Landing Configuration | 58 kias |
Max Range | 775 nm | Takeoff Roll | 860 ft. |
Takeoff Distance Over 50 ft. | 1,490 ft. | Landing Roll | 950 ft. |
Landing Distance Over 50 ft. | 1,050 ft. | ||
Back to Top |
Vulcanair
A-Viator
Base Price | $3.2 million | Typically Equipped Price | N/A |
Engines | Rolls-Royce 250-B17C | Horsepower Per Side | 328 shp |
Propellers | Hartzell (3 blade) | Seats | 10 |
Length | 37 ft. | Height | 11 ft. 11 in. |
Wingspan | 39 ft. 4 in. | Wing Area | 200 sq. ft. |
Wing Loading | 33.07 lb./sq. ft. | Power Loading | 10.08 lb./shp |
Max Takeoff Weight | 6,613 lb. | Empty Weight | 3,858 lb. |
Useful Load | 2,811 lb. | Fuel Capacity | 222 gal./1,4867 lb. |
Max Operating Altitude | 25,000 ft. | Max Rate of Climb | 1,650 fpm |
Single Engine Rate of Climb | 270 fpm | Max Cruise Speed | 214 ktas |
Normal Cruise Speed | 178 ktas | Stall Speed, Landing Configuration | 69 kcas |
Max Range | 939 nm | Takeoff Roll | 1,312 ft. |
Takeoff Distance Over 50 ft. | 2,100 ft. | Landing Roll | 1,083 ft. |
Landing Distance Over 50 ft. | 2,296 ft. | ||
Back to Top |